DEN04LA112 · Swearingen SA-226T
Swearingen SA-226T · Accident: partial loss of engine power (mechanical failure) during takeoff
From Garfield County Regional Airport (RIL) to Acadiana Regional Airport (ARA)
Event
- NTSB case
- DEN04LA112
- Event typeAccident: someone killed or seriously injured, or the aircraft substantially damaged (NTSB definition). Incident: an occurrence that affected or could have affected safety, short of that. Glossary
- Accident
- InvestigationHow far the investigation had got when the record was published: preliminary, ongoing, final or completed. Unknown where the source does not say. Glossary
- Completed
- API-reported fatalities
- 0 · all aircraft and ground
- Ground fatalities
- Unknown
- OperationWhat kind of flying it was, grouped by the rules it flew under: airline (US Part 121), air taxi and commuter (Part 135), general aviation (Part 91 and similar), military or government. Glossary
- General aviation
- WeatherVisual meteorological conditions (VMC): good enough to fly by looking outside. Instrument conditions (IMC): cloud or low visibility, flying by instruments. Glossary
- Visual Meteorological Cond
Swearingen SA-226T
- Aircraft type
- Swearingen SA-226
- Category
- Airplane
- RegistrationThe aircraft's tail number, such as N12345 or G-ABCD. Registrations are reissued, so the same one years apart can be a different aircraft. Glossary
- N84GA
- Operator
- Robert A. Sandberg · private individual
- Onboard fatalities
- Unknown
- Route
- From Garfield County Regional Airport (RIL), Rifle, COTo Acadiana Regional Airport (ARA), Lafayette, LA
- Aircraft age
- Not recorded
- Flight rulesThe regulations the flight operated under: in the US, Part 91 (general aviation), Part 121 (airlines), Part 135 (air taxi and commuter) and others; for flights abroad, the NTSB's coarser commercial or non-commercial code. Glossary
- Part 91: General Aviation
- Phase of flightThe stage of the flight when things started to go wrong: standing, taxi, takeoff, initial climb, en route, maneuvering, approach or landing. Glossary
- Takeoff · roll/run
- First occurrenceThe single coded event the NTSB judges best describes what happened (records from 2008 on). Older records name the first occurrence in the sequence instead. Glossary
- Partial loss of engine power (mechanical failure)
- DamageDestroyed: beyond practical repair. Substantial: damage that affects the structure, performance or handling and normally needs major repair. Minor: less than that. Glossary
- Substantial
Cause areas
- Pilot in command › Aircraft control, not maintained
Approximate · Coordinates from the NTSB case API, which marks them as estimated or does not say; no uncertainty radius is established.
NTSB narrative
The pilot reported that because of the high density altitude, he wanted to do a CAWI (Continuous Alcohol Water Injection) takeoff. At the end of the runway, the pilot brought up the engine power. The pilot said that the right engine came up to 100 percent torque immediately, but the left engine hesitated at 75 percent torque. The pilot said he gave the left engine more power lever and the torque came up to 85 to 90 percent. The pilot began his takeoff roll. At approximately 70 knots, the left engine "surged down" to 70 to 75 percent torque, and the airplane went sharply left of runway centerline. The pilot said he shouted "abort takeoff" and got the airplane aligned with the runway again. The pilot said he told the copilot to turn off the CAWI pumps. The airplane had slowed to 40 knots. The pilot said as he "initiated the power levers to idle and over the gates into the BETA range, the airplane again surged sharply to the left. The pilot said that he and the copilot applied "hard right rudder" to straighten the airplane. The airplane departed the left side of the runway, striking two taxiway signs and a light, and causing substantial damage to the airplane's pressure vessel, the nose gear doors, and the left propeller. A post-accident examination of the left engine showed a sensor wire to the CAWI system was broken. Additionally, it was discovered that the right engine was misrigged causing a delay when the engine was placed in reverse thrust.
Probable cause
the pilot's failure to maintain aircraft control during the aborted takeoff resulting in the airplane departing the runway and striking a runway light and two taxiway signs. Factors contributing to the accident were the broken sensor wire to the left engine's Continuous Alcohol Water Injection System, the misrigged power levers, the runway light ,and the signs.
Verbatim NTSB analysis and probable cause from the NTSB dataset
Sources
NTSB record DEN04LA112
- Event ID
- 20040729X01096
- Case number
- DEN04LA112
- Dataset
- historical-pre2008
- Source SHA-256
- 89e2df6d848e7ab3b42e7d7c7a03ff403303057a26ca04c95b3ea67201c3ce74
Source notes (4)
- Unreviewed is an editorial label, not an investigation status. API-sourced is not report-checked or human-reviewed. Explicit event totals are used without summing aircraft injury tables; onboard allocation is withheld. Unknown values remain unknown. The operation category is mapped from the NTSB-reported FAR part and has not been reviewed.
- Filled from the NTSB case API where the bulk record had no value: investigation status, coordinates. Values present in the bulk record are kept.
- The date is the local date, which is the same as the UTC date the NTSB stores.
- API snapshot SHA-256: f744feb94de25026f7f6eaaebd549eace6ae7934e9fe297de4e3aa9722fcbc44; retrieved 2026-09-22T07:01:08.032Z.